A-CAUTION PANEL Flashcards
0
Q
#1 or #2 STALL SYST FAIL
A
These caution lights come on in flight, when a malfunction that prevents stick shaker and pusher operations are sensed
1
Q
ROLL SPLR
INBD GRND
A
FCECU is not able to control the inboard spoiler lift dump operation. The inboard spoilers do not extend at touchdown or the inboard spoilers extend after the TAXI mode selection after touchdown.
2
Q
FLIGHT DATA
RECORDER
A
This caution light comes you do the FDR test, if the light comes stays on then the FDR test has failed.
3
Q
ELEVATOR
FEEL
A
One of the FCECU channels is not able to control the pitch feel actuator or acceleration 1 and 2 mismatch. Airspeed 1 and 2 mismatch (RUD PRESS, SPLR OUTBD, and PITCH TRIM caution lights will also come on).
4
Q
R AC BUS
A
AC GENS are protected from bus faults by their respective GCU’s. The GCU detects an excessive load and the GCU isolates the affected BUS and the R AC BUS illuminates.
5
Q
PITOT
HEAT 1
PITOT
HEAT 2
PITOT
HEAT STBY
A
These caution lights come on when the related probe has malfunction and or the switch is tuned off
6
Q
ELEVATOR TRIM
SHUTT OFF
PUSH OFF SWITCH ON THE GLARE SHIELD
A
The switch has failed or the elevator trim switch is pressed for more then 3 seconds
7
Q
ICE DETECT
FAIL
A
Both de ice probes have failed
8
Q
FLT COMPT
DUCT HOT
A
Flight compartment supply duct’s temperature is 88C for 190F
9
Q
PITCH
TRIM
(2)
A
- One of the FCECU channels is not able to control its related pitch trim actuator.
- Or the pilot and co pilots trim are different
10
Q
L AC BUS
A
Left AC bus fault is sensed and the GCU has isolated it
11
Q
#1 HYD ISO VLV
A
1 HYD ISO VLV is closed.
- ANTI SKIDS ( BREAKA )
- INBORD SPOILER
12
Q
1 PEC
A
1 Propeller Electronic Controller Malfunction
If the #1 PEC and the associated prop is above 1020rpm then its a prop over speed and vitals apply
13
Q
#1 ENG FUEL PRESS
A
Pressure at the engine driven #1 inlet is low or below a preset value
14
Q
#2 ENG FUEL PRESS
A
Pressure at the engine driven #1 inlet is low or below a preset value
15
Q
2 PEC
A
2 Propeller Electronic Controller Malfunction
If the #1 PEC and the associated prop is above 1020rpm then its a prop over speed and vitals apply
16
Q
CABIN
DUCT HOT
A
Cabin supply duct
temperature is 88 deg
C(190 deg F).
17
Q
#2 HYD ISO VLV
A
No. 2 isolation valve
is closed.
All you have left is ( RE )
- Rudder ( Upper PTU )
- Elevator
18
Q
#2 BLEED HOT
A
No. 2 bleed air supply
duct temperature is hot,
or duct overpressure or
duct leak.
19
Q
#1 BLEED HOT
A
No. 1 bleed air supply
duct temperature is hot,
or duct overpressure or
duct leak.
20
Q
#2 ENG HYD PUMP
A
No. 2 Engine Driven Hydraulic Pump pressure is low or the condition lever is set to the FUEL OFF position.
21
Q
#1ENG HYD PUMP
A
No. 1 Engine Driven Hydraulic Pump pressure is low or the condition lever is set to the FUEL OFF position.
22
Q
#1 STBY HYD PUMP HOT
A
The temperature of the electric motor windings on the No. 1 standby hydraulic pump is too hot.
23
Q
SPLR
OUTBD
A
FCECU has failed to inhibit outboard spoiler pressure at greater than 170 KIAS or has failed to re-enable below 165 KIAS.
The FCECU fails to lockout outboard spoilers when airspeed > 185 KIAS, or fails to enable below 150 KIAS,
• Airspeed # 1 is not equal to Airspeed # 2 ± 17 kt (IAS MISMATCH message on PFD, RUD CTRL, ELEVFEEL and PITCH TRIM caution lights also turn on),
24
```
#2 STALL
SYST FAIL
```
No. 2 stall warning
system malfunction, or
a loss of a valid AOA
parameter.
25
GPWS
```
Ground Proximity
Warning System
(GPWS) has
malfunctioned or there is
an RA failure.
```
26
ELEVATOR
| ASYMMETRY
```
Right and Left elevators
have a difference in
angle of 4° for IAS > 185
KIAS and 6° for IAS
< 185 KIAS.
```
27
DC BUS
```
EPCU has reconfigured
the main 28 VDC
generation sytem
because of a source or
bus fault condition.
```
28
ENG ADPT
| HEAT 1
Malfunction of both
No. 1 air intake heating
elements.
29
ENG ADPT
| HEAT 2
Malfunction of both
No. 2 air intake heating
elements.
30
CABIN
| PACK HOT
Right Air Cycle Machine
(ACM) discharge
temperature is hot.
31
STBY
| BATTERY
Standby battery is not
connected to its main
feeder bus for charging.
32
```
#2 DC GEN
HOT
```
No. 2 DC generator
| temperature is hot.
33
```
#1 DC GEN
HOT
```
No. 1 DC generator
| temperature is hot.
34
#1 DC GEN
```
No. 1 DC generator is
not connected to its bus
because of a source
fault condition. The DC
GEN 1 toggle switch
is set to the OFF
position, or the
external DC power is
energizing the left and
right main feeder
busses.
```
35
#2 DC GEN
```
No. 2 DC generator is
not connected to its bus
because of a source
fault condition. The DC
GEN 2 toggle switch is
set to the OFF position,
or the external DC
power is energizing the
left and right main
feeder busses.
```
36
PUSHER
| SYST FAIL
Stick pusher inhibited by
SPS logic, or stick pusher
SHUT OFF Switchlight
pushed.
37
ELEVATOR
| PRESS
Hydraulic systems 1, 2
and 3 are supplying
pressure to the
elevators.
***VALVE IS STUCK OPEN**
38
L TRU
```
AC secondary feeder
bus is not energized
by its related TRU
because of a source
fault condition or the AC
generator toggle
switches are set to the
OFF position.
```
39
R TRU
```
AC secondary feeder
bus is not energized
by its related TRU
because of a source
fault condition or the AC
generator toggle
switches are set to the
OFF position.
```
40
WSHLD
| HOT
Either the left or right
windshield has
overheated.
41
PROP
| DEICE
```
Time Monitor Control
Unit (TMCU) has
malfunctioned or it has
sensed a malfunction in
the prop deice system.
```
42
FLT COMPT
| PACK HOT
Left Air Cycle Machine
(ACM) discharge
temperature is hot.
43
MAIN
| BATTERY
Main battery is not
connected to its main
feeder bus for charging.
44
```
#1 AC GEN
HOT
```
No. 1 AC generator
| temperature is hot.
45
#1 AC GEN
```
No. 1 AC generator is
not connected to its bus
because of a source
fault condition. The AC
GEN 1toggle switch
is set to the OFF
position, or the external
AC power is on.
```
46
#2 AC GEN
```
No. 2 AC generator is
not connected to its bus
because of a source
fault condition. The AC
GEN 1toggle switch
is set to the OFF
position, or the external
AC power is on.
```
47
```
#2 AC GEN
HOT
```
No. 1 AC generator
| temperature is hot.
48
```
#1 RUD
HYD
```
Hydraulic pressure
to the No. 1 rudder
actuator is low.
49
```
#2 RUD
HYD
```
Hydraulic pressure
to the No. 2 rudder
actuator is low.
50
INBD
| ANTISKID
Inboard antiskid control
unit malfunction or toggle
switch is set to OFF.
51
OUTBD
| ANTISKID
Outboard antiskid
control unit malfunction
or toggle switch is OFF.
52
```
#3 STBY
HYD PUMP
```
```
Direct Current Motor
Pump (DCMP) contactor
has been energized for
more than 60 seconds
on ground.
The #3 system pressure
is below 900 psi.
```
53
WSHLD
| CTRL
Left or right anti-ice
| control malfunction.
54
DEICE
| TIMER
Timer and Monitor Unit
| (TMU) malfunction.
55
L TRU
| HOT
Left TRU temperature is HOT
56
R TRU
| HOT
Left TRU temperature is HOT
57
AUX
| BATTERY
Auxiliary battery is not
connected to its main
feeder bus for charging.
58
```
#1 HYD
FLUID HOT
```
No. 1 reservoir
| temperature is hot.
59
```
#2 HYD
FLUID HOT
```
No. 2 reservoir
| temperature is hot.
60
```
#1 ENG
FADEC
```
No. 1 FADEC has a
| cautionary fault.
61
```
#2 ENG
FADEC
```
No. 2 FADEC has a
| cautionary fault.
62
RUD
| CTRL
```
FCECU has detected a
malfunction, or loss of
hydraulic pressure to
both rudder actuators,
or there is an airspeed
mismatch.
```
Airspeed # 1 is not equal to Airspeed # 2 ± 17 kt (IAS MISMATCH message on PFD and ELEVATOR FEEL,
SPLR OUTBD and PITCH TRIM caution lights will also turn on),
63
FLAP
| DRIVE
Flap drive system fault.
64
LDG GEAR
| INOP
Landing gear sequence
malfunction or the
INHIBIT switch has been
set to INHIBIT.
65
WT ON
| WHEELS
PSEU has sensed a
weight-on-wheels
sensor malfunction.
66
EMER LTS
| DISARMED
Emergency lights are
| not armed.
67
INTERNAL
| DOORS
Flight Compartment
door or internal baggage
door not closed and
latched.
68
SIDE WDO
| HOT
The pilot's side window
| has overheated.
69
DEICE
| PRESS
Airframe deice system
pressure is too low and/
or there is a distributer
valve malfunction.
15 PSI
70
AVIONICS
An avionics no dispatch
condition is sensed,
when the aircraft is on
the ground.
71
```
#1 FUEL
FLTR BYPASS
```
No. 1 fuel filter bypass
| impending.
72
```
#2 FUEL
FLTR BYPASS
```
No. 2 fuel filter bypass
| impending.
73
```
#1 TANK
FUEL LOW
```
No. 1 fuel collector bay
quantity is low.
305 LBS
BRAKES OFF
ENGINE RUNNING
74
```
#2 TANK
FUEL LOW
```
No. 2 fuel collector bay
quantity is low.
305 LBS
BRAKES OFF
ENGINE RUNNING
75
APU
APU FADEC has
sensed a fault and shut
down the APU.
76
FLAP
| POWER
Flap drive system
| failure.
77
NOSE
| STEERING
```
Steering system fault
with nose steering ON,
or system remains
pressurized after steering
switch set to OFF
```
78
FUELING
| ON
Refuel/Defuel access
| panel is open.
79
CABIN
| PRESS
Cabin altitude is more than
| 9,800 feet.
80
CHECK
| FIRE DET
Engine fire, APU fire,
detector loop circuit
malfunction is sensed or
if there is a real fire.
81
SMOKE
Smoke is sensed in the
forward or aft baggage
compartment.
82
TOUCHED
| RUNWAY
Rear outer fuselage
surface has touched
the runway.
83
```
#1 ENG
OIL PRESS
```
No. 1 engine oil
pressure is less than
44 psi.
84
```
#2 ENG
OIL PRESS
```
No. 2 engine oil
pressure is less than
44 psi.
85
STBY
| BATTERY
Standby battery is not
connected to its main
feeder bus for charging.
86
AUX BAT
| HOT
Battery temperature
is more than 71 deg C
(160 deg F).
87
MAIN BAT
| HOT
Battery temperature
is more than 71 deg C
(160 deg F).
88
FUSELAGE
| DOORS
One or more fuselage
doors are not closed
or locked.
89
ROLL SPLR
| OUTBD GND
```
FCECU is not able to
control the inboard
spoiler lift dump
operation. The inboard
spoilers do not extend
at touchdown or the
inboard spoilers extend
after the TAXI mode
selection after
touchdown.
```
90
ROLL SPLR
| INBD GND
```
FCECU is not able to
control the inboard
spoiler lift dump
operation. The inboard
spoilers do not extend
at touchdown or the
inboard spoilers extend
after the TAXI mode
selection after
touchdown.
```
91
ROLL SPLR
| INBD HYD
Hydraulic pressure
to the inboard roll
spoiler actuators is low.
92
ROLL SPLR
| OUTBD HYD
Hydraulic pressure to
the outboard spoiler
actuators is low.
